SERVICE BULLETIN
|
|
- Buck Grant
- 5 years ago
- Views:
Transcription
1 SERVICE BULLETIN Date Released: February 3, 2014 Date Effective: February 3, 2014 Subject: Affected Models: Required Action: Time of Compliance: Cracking in elevator spar web near elevator attach points. All RV-3, 4, 6/6A, 7/7A, 8/8A Flying aircraft Inspect for cracks as described in this document. Stop-Drill cracks (if present) then apply E-00001A and E-00001B Hinge Doubler fix as required to cracked elevator hinge positions. RV-3,4 and 6/6A customers will need to fabricate their own doublers using E-00001A and E-00001B as a guideline. Inspect before further flight. - If no cracks are detected, re-inspect at every annual condition inspection or until E-00001A or E-00001B Hinge Doubler repair has been installed. - If cracks are detected, the E-00001A and E-00001B Hinge Doubler repair must be installed at the cracked hinge position before further flight. Synopsis: Cracks have been found near the rivets attaching the nutplates that hold the elevator rod ends to the E-702 Spar and E-610PP or E-611PP Spar Reinforcement Plates. See Figure 1, Figure 2 and corresponding elevator assembly plans pages. Method of Compliance: NOTE: If cracking has occurred at an outboard hinge position, install a doubler only at that position. If cracking is present at an inboard hinge position, doublers must be installed at both the inboard hinge points. This allows correct positioning of the attach point for the elevator horns. Step 1: Carefully inspect elevator hinge positions around the rivets noted in Figure 2. Page 1 of 8
2 FIGURE 1: ELEVATOR ASSEMBLY Step 2: If cracking is found remove the elevator and stop drill #40 the cracks through the E-702 spar only. Do not continue to drill through the E-610PP or E-611PP Spar Reinf. Plates. This will remove only the material for the drill point from the reinforcement plates. See Figure 2. Page 2 of 8
3 FIGURE 2: INSPECTION FOR CRACKING Step 3: Cut off the head of a SCREW 3/8-24 X 1 3/4 to make a tool to hold the nutplate in place in the following steps. See Figure 3. FIGURE 3: NUTPLATE HOLDING TOOL Page 3 of 8
4 Step 4: Remove the MD3614M Rod End and AN316-6 Jam Nut. Insert the Nutplate Holding Tool into the nutplate. See Figure 5. Step 5: Remove the four rivets surrounding the rod end bearing hole (Figure 2). Use the Nutplate Holding Tool to prevent the nutplate from falling inside the elevator. Step 6: Separate the E Hinge Doubler into A and B parts. See Figure 4. Radius the top and bottom edges of the E-0001A Outboard Hinge Doublers nest against the corresponding radius in the spar. NOTE: If repairing an older non-pre punched kit, AS3-063 can be used to fabricate doublers. Use the supplied doublers as templates for making the new doublers. Leave out the four hole locations where rivets were removed in Step 5. Position the doubler over the nutplate holding tool and match drill the elevator spar and E- 610PP or E-611PP Spar Reinf. Plates at the four corner rivet hole locations. Cleco as you drill each hole. Uncleco the doubler as required then use a hole finder/locator tool to match drill the four original holes into the new doubler while the doubler is clecoed in place. FIGURE 4: SEPARATING THE HINGE DOUBLER Step 7: Final-Drill #30 the holes in the doublers that are common to the holes in the spar for rivets that were removed in Step 5. Step 8: Slip either the E-00001A Outboard Hinge Doubler or E-00001B Inbd Hinge Doubler as required for the hinge position over the Nutplate Holding Tool. Step 9: Cleco the doubler to the Elevator Assembly using the inboard and outboard most holes common between the doubler and open holes from Step 4. See Figure 5. Match-Drill #30 the four corner holes in the doubler into the E-702 Spar and the E- 610PP or E-611PP Spar Reinf. Plate. Use a sharp drill bit and light pressure to minimize the burr on the back side. Step 10: Remove and deburr the doubler and the new holes in the elevator assembly. Prime the doubler if desired. Page 4 of 8
5 Step 11: Cleco then rivet the doubler to the Elevator Assembly using the rivets called out in Figure 5 (Be certain to reattach the nutplate when installing rivets in its associated holes). FIGURE 5: ADDING THE DOUBLER PLATE (SKIN NOT SHOWN FOR CLARITY) NOTE: Steps 12A-C are for elevators that only need a doubler installed at the outboard hinge point. Skip to Step 13 if doublers were installed at an inboard hinge point location. Step 12: Remove the Nutplate Holding Tool and reinstall the MD3614M Rod End and AN316-6 Jam Nut. NOTE: Misalignment of a rod end relative to the overall hinge line of the elevator can contribute to cracking near the misaligned rod end. Step 12A: Adjust the outboard rod end to a distance of 13/16 from the center of the rod end ball to the forward face of the E-00001A Outboard Hinge Doubler. Page 5 of 8
6 Step 12B: Adjust the center rod end so that it is aligned/centered between the hole in the WD-605-L/R-1 Elevator Horn and the outboard rod end. This will cause the outboard end of the elevator to be swept back very slightly. This change is insignificant. To check the alignment, place a white piece of paper outboard of the outboard rod end. Shine a bright light on the paper (works best in a dimly lit room). Sight by eye through the 1/4 inch hinge point hole in the elevator horn and verify that the inboard rod end is centered relative to the hole in the elevator horn and the outboard rod end (the balls in both rod ends need to be positioned as they would be when bolted to the stabilizer). If it is not properly centered, adjust only the inboard rod end as needed. Step 12C: Once the hinge line is straight tighten all jam nuts to secure the rod ends in place. Remount the elevator(s) to the aircraft per the instructions that came with your kit. NOTE: Steps 13A-F are for elevators that have had doubler installed at an inboard hinge position. Step 13: Remove the Nutplate Holding Tool and reinstall the MD3614M Rod End and AN316-6 Jam Nut Step 13A: Adjust all rod ends in both elevators to a distance of 13/16 from the center of the rod end ball to the forward face of the E-00001A or E-00001B Outboard Hinge Doubler (or 7/8 to the E-702 spar web if the outboard doubler has not been installed). Step 13B: Remove the HS-411BPP brackets and VA-146 bearing assembly from the center of the horizontal stabilizer rear spar. Clamp the bearing assembly on top of the supplied AS3-063X2 3/4X3 1/8 and trace the footprint of the brackets onto the sheet. Match-Drill #12 each of the four bracket attach holes into the sheet. This will make a spacer. Use the trace line to cut the spacer to size. Deburr the spacer and prime if desired. Re-install the assembly and spacer to the rear spar using supplied AN3-6A bolts, AN nuts, and NAS1149F0363P washers. Step 13C: Confirm a straight hinge line through all three hinge points as described in Step 12B. Once the hinge line is confirmed straight, tighten all jam nuts to secure the rod ends in place. Page 6 of 8
7 Step 13D: Lengthen the elevator pushrod 1/16 (1.5 turns) while maintaining proper rod end bearing engagement. Step 13E: If applicable, trim the lower aft corner of the WD-605-Elevator Horn as shown in Figure 6. Deburr and prime the trimmed edge. Check that the elevator travel is within the limits given for your aircraft. Step 13F: Remount the elevator(s) to the aircraft per the instructions that came with your kit. Step 14: Make a logbook entry indicating compliance with this service bulletin. FIGURE 6: TRIMMING THE ELEVATOR HORNS Page 7 of 8
8 Note: Repair Kits can be obtained from Van s Aircraft. Order: SB indicates the number of doublers to be installed SB for 2 doublers to be installed SB for 3 doublers to be installed SB for 4 doublers to be installed Important! Order the appropriate Repair Kit from the list above based on the number of doublers to be installed. Parts list: (Single doubler Repair Kit) Qty 1 E SCREW 3/8-24 X 1 3/4 1 AS3-063X2 3/4X3 1/8 4 AN3-6A 4 AN NAS1149F0363P 6 CR (6 per hinge point) 2 CR (2 per hinge point) Note: the number of CR3213 rivets will be adjusted automatically depending on which Repair Kit is ordered. Quantities for the remainder of the parts remain the same in all Repair Kits. Page 8 of 8
SERVICE BULLETIN
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm SERVICE
More informationSERVICE BULLETIN
SERVICE BULLETIN 16-03-28 Date Released: May 6, 2016 (Initial Release) June 2, 2016 (Added Note, pg.11) Date Effective: May 6, 2016 Affected Models: Subject: Required Action: All RV-3, 4, 6/6A, 7/7A, 8/8A,
More informationPage: REV 2: Added "Step 1: Straighten the W-0007B Rear Spar Reinforcement Fork as described on Page 10-03, Step 4."
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
More informationREVISION DESCRIPTION:
REVISION DESCRIPTION: Page: 09-10 REV 1: Delete Step 1. 14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and
More informationHorizontal Stabilizer Service Bulletin
Horizontal Stabilizer Service Bulletin Date: Friday November 19, 2004 To: All Super Rebel/Moose owners Re: Horizontal stabilizer tip rib INFO: A number of Super Rebels have shown cracking on the tip rib/rear
More informationSERVICE KIT. March 22, 2011 Original Issue: January 22, 2001 Page 1 of 7
Single Engine SERVICE KIT TITLE RUDDER STOP MODIFICATION - SHEET METAL BULKHEAD EFFECTIVITY NOTE: Some airplanes in this serial range may have a forged bulkhead installed after leaving the factory. Service
More information77.5 degrees REAR CHANNEL PLYWOOD TEMPLATE
77.5 degrees REAR CHANNEL PLYWOOD TEMPLATE Ref. 6-B-14 Make following template: Vertical distance = 300mm Layout dimensions shown in the bottom right table on drawing 6-B-14 Top and bottom are square to
More informationSERVICE BULLETIN
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm SERVICE
More informationSTOL CH 701. Clamp a reference extrusion on the bottom of the spar. Clamp the bottom flange of the rib to the extrusion. Rear Root Rib 7V4-2
Rear Root Rib 7V4-2 Clamp a reference extrusion on the bottom of the spar. Clamp the bottom flange of the rib to the extrusion. Cleco the root nose rib to the spar Position the rear root rib at station
More informationCut the center and pre-drill the Hinge Plate. Do not drill the Rudder Hinge hole at this time.
7F4-1 Upper Rudder Hinge Plate Layout the cut for the Upper Hinge Plate. Measure and mark the center for the Rudder Hinge. The center hinge hole is 75mm from the back edge of 7F4-1. Cut the center and
More information2.1 Parts List Tool requirement Before you start assembling the Stabiliser Front Spar Center Doublers...
Stabilizer Assembly 2.0 Exploded View...Error! Bookmark not defined. 2.1 Parts List...3 2.2 Tool requirement...5 2.3 Before you start assembling the Stabiliser...6 2.4 Front Spar...6 2.5 Center Doublers...7
More informationSection 6-T-3 Elevator
Section 6-T-3 Elevator This manual has been prepared for assembly of the Elevator using match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
More informationSection 75-ZA-2. Rudder Mounting
Section 75-ZA-2 This manual has been prepared for installation of the Rudder. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy between this manual and
More informationSTOL CH H3-3SP Center Hinge Bracket. IMPORTANT: The Bracket 7H5-3SP is not symmetrical
7H3-3SP Center Hinge Bracket IMPORTANT: The Bracket 7H5-3SP is not symmetrical Using a square helps layout and mark the perpendicular and the hinge hole. Note: Position of 1/4 hinge hole is 115.5mm from
More informationElevator Assembly. To assemble the SR3500 Elevator, you will need the following tools:
Elevator Assembly To assemble the SR3500 Elevator, you will need the following tools: 1. Drill 2. Tape Measure 3. Felt Marker 4. #40, #30, 3/16, #11 Drill Bits 5. #40, #30 and 3/16 Clecos 6. Cleco Pliers
More informationPhoto-Guide (ZE & ZE )
Photo-Guide (ZE-2009-05 & ZE-2009-07) The following photo-guide is for educational purposes only. It is intended to assist owners and/or aircraft mechanics with the installation of elements from from 6Z-1G
More informationPage: REV 1: Step 5 and Figure 5 updated to better describe the potential necessity of modifying a rivet squeezer yoke.
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
More information75-TA-4. Elevator Skins
75-TA-4 This manual has been prepared for assembly of the. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy between this manual and the drawings, the
More informationSECTION 11: EMPENNAGE ATTACHMENT
TILCONE V-STB VS-1204 FWD SKIN SECTION 11: EMPENNGE TTCHMENT RUDDER STBILTOR RIGHT ST LEFT ST DTE OF COMPLETION: PRTICIPNTS: 09/25/08 0 RV-12 DTE: REVISION: PGE 11-01 Step 1: Remove the VS-1204 Fwd Skin,
More informationSTC GROUP LLC Page Ruddiman Drive PA-28 & PA-32 Trio Pro Pilot Installation Instructions North Muskegon, Michigan 49445
STC GROUP LLC Page 1 STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 DOCUMENT NO: 1028001 REVISION D TRIO PRO PILOT INSTALLATION INSTRUCTIONS PIPER AIRCRAFT CORPORATION PA-28 AND PA-32 DATE:
More informationREAR FUSELAGE ASSEMBLY
SECTION 2 Rear Fuselage Bottom Assembly Ref Dwg 8FR-2 SECTION 2 - Page 1 of 17 FUSELAGE BOTTOM SKIN 8F2-3A Note: The edges of skin 8F2-3A are not a straight line. Check: edge distance from the center of
More informationFlaperon Assembly Manual
Flaperon Assembly Manual for PegaStol Aftermarket Wings A Senior Project presented to The Faculty of the Aerospace Engineering Department California Polytechnic State University, San Luis Obispo In Partial
More informationSERVICE BULLETIN. No. SB-AG-45 Rev. B JUNE 1, 2007 FIN SPAR & ATTACH FITTINGS INSPECTION AND UPGRADE IMPORTANT:
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-883-1440 ext. 341 FAX 229-436-4856 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-45 Rev. B JUNE
More informationAmerican Champion Aircraft Corp. Rochester, WI Page 1 of 5
Service Letter: 444 Initial Revision Date: August 18, 2017 Title: American Champion Aircraft Corp. Rochester, WI 53167 Page 1 of 5 Installation of Aileron Hinge Reinforcement Models: 8KCAB serial numbers
More informationFLAP AILERON FLAP / FUSE SEAL KIT
FLAP AILERON FLAP / FUSE SEAL KIT APPLICABLE MODELS BEECHCRAFT MODELS 33/35/36 I N S T A L L A T I O N M A N U A L I S S U E D A T E 06/06/84 KNOTS 2U, LTD. 709 AIRPORT ROAD BURLINGTON, WI 53105 262 763-5100
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: G REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: G-1006-51 REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 WITH PREVIOUS CESSNA EQUIPPED AUTO PILOT DATE: Original Issue
More informationThree vertical L angles must be riveted to each main spar (length = 206mm see boxed diagram on drawing 7-V-2).
Cut over-sized (left); Trim and file (above). Note: Six needed. Three vertical L angles must be riveted to each main spar (length = 206mm see boxed diagram on drawing 7-V-2). Trace line down center of
More informationINSTALLATION INSTRUCTIONS FOR EXHAUST CUFF MODIFICATION
INSTALLATION INSTRUCTIONS FOR EXHAUST CUFF MODIFICATION Document # PCA1001-21 Revision LTR: NC Date: 09/15/08 1 Notes: 1. The Exhaust Cuff comes assembled with the three attachment brackets secured. We
More informationREVISION DESCRIPTION:
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
More informationCENTER WING SECTION (CWS) WORK REPORT
CENTER WING SECTION (CWS) WORK REPORT No. Check Parts / Description Qty PHASE 1: Preparations 1 [ ] 6V1-3 Rear ribs 2R & 2L 1 [ ] L Angle 6 2 [ ] 6V2-1 Rear Ribs.032 2R & 2L 2 [ ] 6V5-1 Gear Rib Doubler
More informationSTOL CH 701. Standard L ANGLES are supplied in 4ft length. Ref. bottom left diagram on drawing 7-V-2
Standard L ANGLES are supplied in 4ft length. Ref. bottom left diagram on drawing 7-V-2 Length = 206mm. Layout the cut line on the outside flanges. Ref. see boxed diagram on drawing 7-V-2 Three vertical
More informationSection 75-AA-1. Flaperon Assembly
Section 75-AA-1 This manual has been prepared for assembly of the flaperons supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
More informationSection C75-WA-1. Wing Skeleton
Section C75-WA-1 This manual has been prepared for assembly of the wing skeleton supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any
More informationSTOL CH 701. Layout the cut line along the bend tangent line on the web. 7V6-1 and 7V6-2SP
Layout the cut line along the bend tangent line on the web. 7V6-1 and 7V6-2SP ORIENTATION: 90 degree flange is up Layout the bend line, 20mm from the end. Ref. bottom right diagram 7-V-6 Use a square to
More information9.3 FUSELAGE ASSEMBLY 14/03/02
9.3 MATING THE TAIL CONE TO THE CABIN 1) Trim the bottom flange of both FUS-339 side skins on the tailcone assembly as in Figure 1. 2) Remove the bottom two RBULK 2A s of bulkhead A on the tailcone. 3)
More informationIMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17
IMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17 (This Service Letter is FAA. Approved) DATE: OCTOBER 24, 1959 SUBJECT: REAR BULKHEAD
More informationSERVICE BULLETIN SB-GL12-01R GREAT LAKES AIRCRAFT HORIZONTAL STABILIZER SPAR INSPECTION COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND:
SUBJECT: AFFECTED MODELS: 2T-1A 0501 and 0502 2T-1A-1 0503 through 0699 2T-1A-2 0701 through 1012 COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND: Released: 01/25/2012 Page 1 of 5 HORIZONTAL STABILIZER
More information11) Chromate the mating surfaces of the Leading edge Root Rib, Doubler and Root Rib Stiffeners. Rivet together with 1/8 rivets (RV-1410).
11) Chromate the mating surfaces of the Leading edge Root Rib, Doubler and Root Rib Stiffeners. Rivet together with 1/8 rivets (RV-1410). 12) Chromate the Root Rib Attach Bracket and rivet to the Root
More informationZODIAC 601 XL. ZODIAC CH 601 Series. Parts are labeled for easy identification with a part number and description:
CH 601 Series Parts are labeled for easy identification with a part number and description: Part number example: 6T4-4 Vertical Tail Spar 6 - Zodiac CH 601 model T - Rudder section of the Aircraft drawings.
More informationSection 6-B-6, 6-B-7, & 6-B-8 Firewall Assembly
Section 6-B-6, 6-B-7, & 6-B-8 Firewall Assembly This manual has been prepared for assembly of the firewall supplied with match drilled parts. This photo assembly manual is intended as a supplement to the
More informationSTOL CH 801 SECTION 2: Nose Rib 8R1-7
SECTION 2: Nose Rib 8R1-7 Position the lower nose rib on the front of the spar at the predrilled holes just above rear rib #3 (615mm from the bottom of the spar) Check lateral alignment (rib is centered
More informationSection 75-FA-5. Firewall Assembly
Section 75-FA-5 This manual has been prepared for assembly of the firewall supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
More informationChap. 9.2 SR3500 Fuselage Assembly - Cabin. MODEL: SR Murphy Aircraft Mfg. Ltd. All rights reserved.
26/06/2006 Page 1 26/06/2006 Page 2 26/06/2006 Page 3 Parts List for Gear Box No. Part Number Description Qty Required 1,23 FUS0711QL BRACING CHANNEL 2 2,22 FUS0711QR BRACING CHANNEL 2 3 FUS301QB CARRYTHROUGH
More informationSERVICE BULLETIN. SERIAL NUMBERS thru A0001 thru 402A B0001 thru 401B thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 401 401-0001 thru 401-0322 401A 401B 401A0001 thru 401A0132 401B0001 thru 401B0221 402 402-0001 thru 402-0322
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN REPORT NO: REVISION H
STC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN 49445-2783 REPORT NO: 1006004 REVISION H TRIO AUTO PILOT PROVISIONS INSTALLATION INSTRUCTIONS 1953 CESSNA 180 THROUGH 1962 180E 1956 CESSNA 182
More informationCathy and Phil Cobbin's RV7A Project 2003 Photo Log
Cathy and Phil Cobbin's RV7A Project 2003 Photo Log 1 of 60 2003 09 22 Arrival of the empennage kit 2 of 60 2003 09 23 Cleco horizontal stabilizer rear spar together to file/fit the radius to clear the
More information2000 Tomlynn Street P.O. Box 6861 Richmond, Virginia / FAX 804/ Service Bulletin
Sequoia Aircraft Corporation 2000 Tomlynn Street P.O. Box 6861 Richmond, Virginia 23230 804/353-1713 FAX 804/359-2618 Service Bulletin Service Bulletin No. 93-1 Subject: Flap Flutter Date: June 24, 1993
More informationSTOL CH st Edition 1 st Revision Drawings Summary of changes from Edition 1 to Edition 1 Revision 1.
STOL CH 750 1 st Edition 1 st Revision Drawings Summary of changes from Edition 1 to Edition 1 Revision 1. Page Date Drawing Title 75-G-0 01/10 Three View Drawing 75-G-1 01/10 Drawings Index 75-RX-1 05/09
More information105" TIGER MOTH ARF INSTRUCTION MANUAL VERSION 1.0
105" TIGER MOTH ARF INSTRUCTION MANUAL VERSION 1.0 Step 1. Installation of the aileron servos 1) Mount aileron servo to servo mounting blocks with servo s screws. Install servo mounting plate with screws.
More information16. Wing Final Assembly and Installation
Section Objective: Installation and rigging of ailerons. Pitot tube install, and any other wing related items. Required Parts: Left aileron push rod ALA-0072, Right aileron push rod ALA-0073, Push tube
More informationSTANDARD CANOPY WORK REPORT B-1
STANDARD CANOPY WORK REPORT B-1 No. Check Parts / Tools Qty _ Canopy Lock 1 [ ] 6E2-3 Canopy Hinge Block 1 2 [ ] 6E4-5 Canopy Side Frame 2 2 [ ] 6E2-1 Canopy Lock Assembly 1L + 1R 3 [ ] 6E2-4 Rear Lock
More information12. Wings, Flaps, Ailerons and Struts
12. Wings, Flaps, Ailerons and Struts Fit Aileron Hinges Reference: Drawing 20270K2 Photo 12.1 Parts Required: 2007092 Aileron LS 200809N Aileron RS 2001394 Hinge 3/16 A1 (4) 2001694 Hinge Pin (4) PH0059N
More informationWING ASSEMBLY 23.5 (Continued)
A VERY IMPORTANT NOTE found on many wing drawings states Do not drill any unspecified holes into spar. This is extremely important as any extra holes may, under extreme conditions, WEAKEN THE SPAR. Note;
More informationZODIAC CH650. ZODIAC CH 650 Series. Parts are labeled for easy identification with a part number and description:
CH 650 Series Parts are labeled for easy identification with a part number and description: Part number example: 6T4-4 Vertical Tail Spar 6 - Zodiac CH 650 model T - Rudder section of the Aircraft drawings.
More informationZODIAC CH 601 Series Kit Aircraft
ZODIAC CH 601 Series Kit Aircraft THE FOLLOWING IS A DRAFT MANUAL This manual has been written and published strictly for informational purpose. It has been prepared as a guide to facilitate the assembly
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO REVISION D TRIO AUTO PILOT INSTALLATION INSTRUCTIONS
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO. 1006003 REVISION D TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 WITH CESSNA NAVOMATIC EQUIPPED AUTO PILOT DATE: Original
More informationSUBJECT: HORIZONTAL STABILIZER SUPPORTS ALL, INSTALLATION OF.
TECHNICAL BULLETIN 206L-00-203 25 August 2000 Revision B, 27 October 2014 MODEL AFFECTED: 206L, 206L-1, 206L-3 and 206L-4 SUBJECT: HORIZONTAL STABILIZER SUPPORTS 206-023-131-ALL, INSTALLATION OF. HELICOPTERS
More informationSection 75-FA-2 Top Fuselage Skin & Rear Fuselage Assembly
Section 75-FA-2 Top Fuselage Skin & Rear Fuselage This manual has been prepared for assembly of the rear fuselage supplied with match drilled parts. This photo assembly manual is intended as a supplement
More informationZODIAC CH 601 Series Kit Aircraft
ZODIAC CH 601 Series Kit Aircraft THE FOLLOWING IS A DRAFT MANUAL This manual has been written and published strictly for informational purpose. It has been prepared as a guide to facilitate the assembly
More informationWARNING Honda Pilot Installation Instructions BX2244. Serial Number
Please read BOTH these and the General Instructions before attempting to install or operate this equipment. Serial Number 1. Blue Ox towing products and accessories are intended to be installed by Blue
More informationZODIAC 601 XL UPRIGHT CHANNELS 6B5-6. Top and bottom outboard flange is joggle to overlap the.093 extrusion 6B2-3 and 6B11-1
UPRIGHT CHANNELS 6B5-6 Top and bottom outboard flange is joggle to overlap the.093 extrusion 6B2-3 and 6B11-1 Length: fits between the bottom and top longerons. Clamp the upright channel to the rear frame
More informationCh. 9.0 ELITE FUSELAGE ASSEMBLY 14/02/2003
Fuselage Assembly In the front of the fuselage manual you will find an exploded view of the fuselage and a side view schematic. We suggest that you tape these to the wall of your workshop. Refer to them
More informationSECTION 34: C-1206 GUIDE PLATE C-656 CANOPY HANDLE WD-1218 CANOPY LATCH
VAN'S AIRCRAFT, INC. SECTION 34: C-1206 GUIDE PLATE C-656 CANOPY HANDLE WD-1218 CANOPY LATCH CANOPY INSTALLATION C-1203B ATTACH ANGLE C-1201 CANOPY C-1205 LATCH BLOCK C-1202 CANOPY SKIRT C-1203A ATTACH
More informationWING ASSEMBLY SECTION 4. Mounting Wing Ribs to Main Spar. 1. Identify the proper locations for those ribs with attachment brackets.
WING ASSEMBLY SECTION 4 Mounting Wing Ribs to Main Spar Compass Check 1. Identify the proper locations for those ribs with attachment brackets. 2. Position and drill the nose ribs. 3. Un-cleco the nose
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: 1006003 REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 DATE: Original Issue 10 July, 2017 WRITTEN BY: Paul Odum APPROVED
More informationFord Pick Up Rear leaf Spring Kit Installation Instructions
1948-1956 Ford Pick Up Rear leaf Spring Kit Installation Instructions 1-800-984-6259 www.totalcostinvolved.com Parts 48 inch leaf (2) springs (4) U-bolts 3/8-24 x l 1/4bolts (16) & nuts (2) 1/2-20 x 4
More informationZODIAC 601 XL. REAR RIBS 6W6-1 to 6W6-9. Reference to drawing 6-W-00 for orientations of ribs flanges. Rear ribs are tapered: rib #9 is the shortest.
REAR RIBS 6W6-1 to 6W6-9 Reference to drawing 6-W-00 for orientations of ribs flanges. Rear ribs are tapered: rib #9 is the shortest. Right wing Zodiac CH 6-W-6 - Page 1 of 12 Burr on edge of flanged lightening
More informationWARNING. Baseplates. Serial Number
Baseplates Serial Number Attachment Tab Height: 13.5 Attachment Tab Width: 24 Please read BOTH these Installation Instructions and the General Towing Instructions before attempting to install or operate
More informationSERVICE BULLETIN. SERIAL NUMBERS thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 425 425-0001 thru 425-0236 Customers have requested an access panel to gain easy access to the forward spar
More informationRangerWare Fiberglass Door System Installation Instructions P/N
Page 1 of 9 RangerWare Fiberglass Door System Installation Instructions P/N 2878016 ORDER OF INSTALLATION Note: To assure proper order, read all Accessory Installation Instructions before beginning. 1.
More informationNOTE KIT CONTENTS. 21 NOV 2012 KI / KI Revision D R44 Five-Point Harness Inst l Kit Page 1 of 9. Zach Archer / Lindsay Allen / Pat Cox
KI-155-1 R44 Standard to Five-Point Harness Installation Kit Instructions & KI-155-2 R44 Four-Point to Five-Point Harness Installation Kit Instructions NOTE Visit www.robinsonheli.com to verify kit instructions
More informationFAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT. Eyebrow Window Replacement
FAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT AIRPLANE MAKE: Boeing AIRPLANE MODEL: 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900 TO BE ADDED TO AMM CHAPTER 56-11-XX This
More informationREAR FUSELAGE ASSEMBLY
SECTION 5 Tail Attachments on Fuselage Ref Dwg 8RU-3 The rudder hinge line (HL) is parallel to the aft edge of the fuselage skin SECTION 5 - Page 1 of 9 Looking at the top of the rear fuselage. Stabilizer
More informationDodge Dakota WARNING. B as e plate s. Installation Instructions BX1971. Serial Number
B as e plate s BX1971 Serial Number Attachment Tab Height: 17.5 Attachment Tab Width: 20 Please read BOTH these Installation Instructions and the General Instructions before attempting to install or operate
More informationSTOL CH nd Edition Drawings July 20, 2010 Summary of changes from Edition 1 to Edition 2.
STOL CH 750 2 nd Edition Drawings July 20, 2010 Summary of changes from Edition 1 to Edition 2. Page Date Drawing Title 75-G-0 07/10 Three View Drawing 75-G-1 07/10 Drawings Index 75-G-2 03/10 General
More informationZODIAC 601 XL. Detail of outboard end. Full length recessed elevator trim tab. Detail of inboard end. Trim tab along left trailing edge of elevator.
Full length recessed elevator trim tab. Detail of outboard end. Detail of inboard end. Trim tab along left trailing edge of elevator. Trim tab in neutral position 6-T-6 - Page 1 of 12 Drill out the middle
More informationFORWARD FUSELAGE SIDES & REAR TOP SKINS
FORWARD FUSELAGE SIDES & REAR TOP SKINS WORK REPORT Step No. Check Parts / Tools Qty Preparations. 1 [ ] 6F5-3 Upper Front Longerons 2 2 [ ] 6F5-5 Heel Support 1 3 [ ] 6F5-2 Front Floor Skin 1 3 [ ] Firewall
More informationSection 6-B-4 Rear Fuselage Riveting
Section 6-B-4 Rear Fuselage Riveting This manual has been prepared for assembly of the rear fuselage. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
More informationIN20733 Rev. B 1/06/2016
14,000 LBS. (6350 Kg.) Bolt-on Alignment Kit Installation Instructions S100129, S100130, S100131 S100132, S100133, S100134 S100135, S100136, S100137, S100173, S100174 Model Max Wheel Base Max 2 Wheel Alignment
More information10. Wing prep and subassembly
Date Section Objective: Construct and fabricate the sub-assemblies of the wing panel. Required Parts: Wing left 11gal PN104-300, Wing right 1gal PN104-400, Wing left 15 gal option PN104-322, Wing right
More informationSection C75-FA-2 Top Fuselage Skin & Rear Fuselage Assembly
Section C75-FA-2 Top Fuselage Skin & Rear Fuselage This manual has been prepared for assembly of the rear fuselage supplied with match drilled parts. This photo assembly manual is intended as a supplement
More informationPLEASE READ THIS NOTICE BEFORE BEGINNING ANY PHASE OF INSTALLATION!!!!
PLEASE READ THIS NOTICE BEFORE BEGINNING ANY PHASE OF INSTALLATION!!!! This kit is designed to be installed by someone with a fair amount of mechanical aptitude. However, if you are not comfortable making
More informationV nyl Gazebo truct c it Assembly Instr ons
V nyl Gazebo Vi Assembly Instr ct tr t u ru ons ct c i ti Pre-assembly Instructions A C B #1 - Site properly prepared. 4" - 6" clean stone 9 linear blocks 2" x 8" x 16" C C A A B B #1a - 12" sauna tubes,
More informationMetal Aircraft Landing Light Installation Instructions
Metal Aircraft Landing Light Installation Instructions This landing light kit was designed for the Thorp T-18 as a method of installing a halogen landing light in the leading edge of the outer bay of the
More information6625 WEST WILSHIRE BLVD. OKLAHOMA CITY, OK (405) FAX (405)
INSTALLATION INSTRUCTIONS FOR THE TAILGATE WITH LATCH AND LINK ASSEMBLY 76-87 FORD SHORT & 53-87 FORD LONG FLARESIDES 1. Assemble the bed and make sure the box is square. Measure the distance between the
More information`48-`56 Ford Pickup Rear leaf Spring Kit Installation Instructions Tech Line:
`48-`56 Ford Pickup Rear leaf Spring Kit Installation Instructions Tech Line: 1-855-693-1259 www.totalcostinvolved.com CHECK ALL PARTS INCLUDED IN THIS KIT TO THE PARTS LIST BEFORE INSTALLING THE KIT.
More informationBX3230 Installation Instructions Oldsmobile Silhouette Chevy Venture
BX3230 Installation Instructions 1997-2004 Oldsmobile Silhouette 1997-2003 Chevy Venture Serial No. The headlight assembly, front fascia, horn bracket and windshield washer reservoir are removed for baseplate
More informationINSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Trans4mer Grille Guard/Winch Mount Kit 37133 (Black) for Ford Ranger As you read these instructions, you will see NOTES, CAUTIONS and WARNINGS. Each message has a specific purpose.
More informationSection 75-SA-1 Slat Section
Section 75-SA-1 Slat Section This manual has been prepared for assembly of the slat sections supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If
More informationPlease read BOTH these Installation Instructions and the General Towing Instructions before attempting to install or operate this equipment.
2005-08 Pontiac G6 GT Please read BOTH these and the General Towing Instructions before attempting to install or operate this equipment. 1. Blue Ox towing products and accessories are intended to be installed
More informationBX1965 Installation Instructions 2004 Chrysler Sebring Convertible
BX1965 Installation Instructions 2004 Chrysler Sebring Convertible Serial No. The headlight assembly, front fascia, horn bracket and windshield washer reservoir are removed for baseplate installation.
More informationSuper Sky Surfer 2000 Assembly Instructions
Super Sky Surfer 2000 Assembly Instructions Note: Plug and Play version of the Sky Surfer comes with fuselage pre-glued and motor/servos installed. If you wish to route antennas or wires through the tail,
More informationWARNING. B as e plate s Jeep Cherokee Jeep Comanche Jeep Wagoneer & LTD Installation Instructions BX1110.
B as e plate s Serial Number BX1110 1984-2001 Jeep Cherokee 1984-92 Jeep Comanche Attachment Tab Height: 14 Attachment Tab Width: 24 Please read BOTH these Installation Instructions and the General Towing
More informationPost-Paint>Fuselage>Interior>Controls>Fit rudder pedals
Post-Paint>Fuselage>Interior>Controls>Fit rudder pedals Objectives of this task: To fit the rudder pedals and steering links to the aircraft, and fit the rudder cable to the rudder pedals and set the deflection
More informationPlease read BOTH these Installation Instructions and the General Instructions before attempting to install or operate this equipment.
Please read BOTH these and the General Instructions before attempting to install or operate this equipment. 1. Blue Ox towing products and accessories are intended to be installed by Blue Ox Dealers who
More informationPROVEN WORLDWIDE SNORKEL FOR CHEVY COLORADO NEW PRODUCT
AEV30272AC Last Updated: 10/09/18 PROVEN WORLDWIDE SNORKEL FOR CHEVY COLORADO NEW PRODUCT Please visit www.aev-conversions.com to view the most current installation guide for this product. This is a new
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN REPORT NO: REVISION A
480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN 49445-2783 REPORT NO: 1006007 REVISION A TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 180F & LATER, CESSNA 185 ALL MODELS NO PREVIOUSLY INSTALLED FACTORY
More informationINSTALLATION INSTRUCTIONS 3 BULL BAR 99-04, 04 "HERITAGE" F-150/250LD 2WD, 97-04, 04 "HERITAGE" 4WD WD EXPEDITION/ WD EXPEDITION PART
INSTALLATION INSTRUCTIONS 3 BULL BAR PART #B-F1971;B-F2971 PARTS LIST: 1 Bull Bar 2 12-1.75mm x 130mm x 40mm Hex Bolts 1 Driver/Left Mounting Bracket 4 12-1.75mm x 35mm Hex Bolts 1 Passenger/Right Mounting
More information8mm x 25mm "Z" Bolt Plates. (2) Tube Spacers. (2) 12mm Bolt Plates w/ Nut
PARTS LIST: 1 Grille Guard 10 12mm Lock Washers 1 Driver/Left Side Frame Mounting Bracket 8 12mm Hex Nuts 1 Passenger/Right Side Frame Mounting Bracket 2 10-1.50mm x 25mm Button Head Bolts 1 Driver/Left
More informationService Bulletin No: Ref No: 136 Modification No: INSPECTION ATA Chapter: 57
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 57-015 Ref No: 136 Modification No: INSPECTION ATA Chapter: 57 WING - AILERON INSTALLATION INSPECTION OF THE AILERON OUTBOARD-BEARING SUPPORT
More information